AD/VAT/4 - Outboard Elevator and Tailplane Hinge - Inspection
1AD/VAT/4 - Outboard Elevator and Tailplane Hinge - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/VAT/4 - Outboard Elevator and Tailplane Hinge - Inspection.
meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0
?xml version="1.0" encoding="utf-8" standalone="no"?>
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Victa and A.E.S.L. Airtourer Series Aeroplanes
AD/VAT/4 Outboard Elevator and Tailplane Hinge - Inspection 3/63
Applicability: Victa Airtourer 100 and 115 with S/Nos. 1 to 14 not incorporating Mod. B27.
Requirement: Inspect the outboard elevator and tailplane hinge fittings P/N 0221012 and 0220009 for cracks, particularly in the region of the bend radius on the elevator hinge P/N 0221012.
Compliance: At intervals not exceeding 25 hours time in service, after 1 September 1971.